JASC 2750

Service difficulty reports · 10,201

Reports filed under 2750 · Trailing Edge Flap Control System, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '2750'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR F3LA00116Carriage · corrodedDEN - FOUND DURING C-7 CHECK INSPECTION, FOUND PITTING CORROSION ON LT INBOARD MID-FLAP OUTBOARD CARRIAGE ON INSIDE DIAMETER OF TORQUE TUBE HOLES. MAINTENANCE REPLACED LT INBOARD MID FLAP OUTBOARD CARRIAGE ASSY. (M)Jun 1, 2000 · N270FL · Boeing 7372L9SDR USAASB00153Flap · jammedTPA - FLT 2797 - AS AIRCRAFT WAS BEING CONFIGURED FOR FINAL APPROACH TO TPA, THE RIGHT INBOARD TRAILING EDGE FLAP BECAME JAMMED WHEN THEY WERE MOVED FROM 10-15 DEGREES. CREW ACCOMPLISHED PROCEDURES AND A GO-AROUND AND DECLARED AN EMERGENCY. FLIGHT LANDED WITJun 1, 2000 · N268AU · Boeing 7372B7SDR AU000440Controller · faulty(AUS) FLAPS FAULTY. FLAPS CHECKED ON GROUND AND OPERATED WITHOUT FAULT.May 31, 2000 · Bac 146200ASDR COMA0060466Power Unit · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FLAP POWER DRIVE UNIT.May 31, 2000 · N783CA · Cndair CL6002B19SDR LR7A0053Jackscrew · wornDURING APPROACH FOR LANDING AT WSAP FLAPS STOPPED AT 60% DURING EXTENSION. CONTINUED APPROACH AND LANDED WITHOUT INCIDENT.DURING SCHEDULED B1 CHECK ACCOMPLISHED VISUAL INSPECTION OF ALL FLAP TORQUE SHAFT CONNECTIONS AND ASYMETRIC BRAKE ASSY. NO DEFECTS NOTEDMay 29, 2000 · N405LC · Lkheed 382GSDR COMA0060461Bpsu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU.May 27, 2000 · N807CA · Cndair CL6002B19SDR VNAA0005011Control Box · failedDURING TAKEOFF THE CREW RECEIVED A FLAP CONTROL FAIL CAS MESSAGE. THE CREW THEN ABORTED TAKEOFF. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL BOX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-50-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT May 26, 2000 · N439JS · Dorner DO328100SDR COMA0060460Fcu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FECU.May 26, 2000 · N963CA · Cndair CL6002B19SDR COMA0060459Warning System · activatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.May 26, 2000 · N963CA · Cndair CL6002B19SDR COMA0060458Bpsu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU.May 26, 2000 · N807CA · Cndair CL6002B19SDR DL72S001028Flap Track · corrodedINBOARD FLAP, NR 5 INBOARD TRACK CORROSION FOUND ON MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, THE SPACER BAR ATTACH BOLT HOLE, AND THE TOGGLE DETENT HOLE. REPAIR PER ER/A 387640-14AD AND BFGOOFRICH ENGINEERING REPAIR NR 23-0801.May 25, 2000 · N531DA · Boeing 727232SDR COMA0060450Warning System · failedFLAPS FAILED AT 26 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.May 24, 2000 · N989CA · Cndair CL6002B19SDR COMA0060449Ecu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FECU.May 24, 2000 · N812CA · Cndair CL6002B19SDR ASOA00059Power Unit · inoperativeFLT 4444 - ON DOWNWIND FOR RUNWAY 22 AT 210 KTS, CREW SELECTED FLAPS TO 8 DEGREES AND FLAPS FAIL MESSAGE APPEARED ON EICAS. CREW FOLLOWED PROCEDURES AS LAID OUT IN ABNORMAL SECTION OF QRH PAGE 8-8. CREW INFORMED ATC OF SITUATION, DECLARED AN EMERGENCY, AND RMay 23, 2000 · N827AS · Cndair CL6002B19SDR QXEA0001583Universal Joint · wornYYC- LEFT HAND WHEEL BAY FLAP DRIVE TUBE U JOINT IS WORN. REPAIRED IAW FOKKER SRM 27-51-04.May 23, 2000 · N480AU · Fokker F28MK4000SDR COMA0060447Warning Light · illuminatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.May 22, 2000 · N785CA · Cndair CL6002B19SDR COMA0060441Flap · malfunctionedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.May 21, 2000 · N963CA · Cndair CL6002B19SDR ASOA00062Connector · inoperativeFLT 4538 - CLIMBING THROUGH 21,000 FEET, CREW RECEIVED A FLAP FAIL MESSAGE. CREW PERFORMED FLAPS FAIL PROCEDURE AND CALLED ATL FLIGHT CONTROL. CREW THEN DECLARED AN EMERGENCY AND RETURNED TO ATL. CAPTAIN SAFELY PERFORMED A ZERO DEGREE FLAP LANDING. MAINTENMay 19, 2000 · N855AS · Cndair CL6002B19SDR 20000608SH013Housing · contaminatedUNIT WAS NOTED TO BE ROUGH IN OPERATION CAUSED FROM CONTAMINATED MIL-H-5606 FLUID. THE NON-STANDARD SLEEVE REPAIR TO HOUSING, COMMON TO THE BORE FORE BEARING, WAS FOUND ROTATING IN THE HOUSING. THIS CAUSED THE FLUID TO BECOME CONTAMINATED WITH ALUMINUM. (X)May 19, 2000 · Boeing 737*SDR QXEA0001359Flap Track · corrodedPDX- RIGHT HAND WING NR 1 FLAP TRACK TOP SURFACE OF THE LOWER RAIL HAS SURFACE CORROSION. REPAIRED IAW RD 8-57-985.May 19, 2000 · N360PH · Dhav DHC8202SDR CA000530074Wire · chafed(CAN) DURING CLIMB, THE FLAP CONTROL CIRCUIT BREAKER TRIPPED AS THE FLAPS WERE BEING RETRACTED. THE BREAKER WAS RESET AND IT TRIPPED AGAIN. THE FLIGHT WAS CONTINUED WITH THE FLAPS PARTIALLY EXTENDED. MAINTENANCE PERSONNEL FOUND THE FLAP CONTROL CIRCUIT WIRINMay 18, 2000 · Cessna S550SDR QXEA0001357Flap Track · corrodedPDX- LEFT HAND FLAP TRACK OUTBOARD VERTICAL, SMALL PIT ON FORWARD SECTION OF TRACK. REPAIRED IAW RD 8-57-1168.May 18, 2000 · N360PH · Dhav DHC8202SDR QXEA0001356Flap Track · corrodedPDX- LEFT HAND FLAP TRACK OUTBOARD VERTICAL, SMALL PIT ON FORWARD SECTION OF TRACK. REPAIRED IAW RD 8-57-1167.May 18, 2000 · N360PH · Dhav DHC8202SDR TSAA0027136Transmitter · malfunctionedFLT 91 - OGG-HNL - DURING TAKEOFF FROM OGG, THE STALL WARNING STICK SHAKER BEGAN AT ROTATION AND WAS CONTINUOUS THROUGH 1000 FEET AND INTERMITTENT AFTER THAT. RETURNED TO OGG FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT TRAILING EDGE FLAP POSITION TRANSMITTMay 17, 2000 · N804AL · Boeing 7372Q9SDR AU000415Wire Rope · worn(AUS) FLAP SECONDARY DRIVE OUTER CABLE SWAGED COUPLING FLANGE WORNEXCESSIVELY.May 16, 2000 · Dhav DHC8102SDR GAIA00278Switch · inoperativeDEN/OAK - FLT 2026 - AFTER FLAP RETRACTION, THE NR 2 LEADING EDGE DEVICE DID NOT INDICATE RETRACTED. AMBER LIGHT REMAINED ON. THE CREW RETURNED TO DEN AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED LEADING EDGE FLAP POSITION SWITCH AND OPMay 14, 2000 · N6838 · Boeing 727223SDR COMA0060420Fcu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FECU.May 14, 2000 · N783CA · Cndair CL6002B19SDR 00FDEA00328Flap · stuckDURING NORMAL FLAPS EXT AT SLC, FLAPS STUCK IN FULL UP POSTION. SYS 1 & 2 FLAP FAULT LIGHT ON.May 12, 2000 · N452FE · Airbus A310222SDR COMA0060407Flap · failedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.May 7, 2000 · N920CA · Cndair CL6002B19SDR CA000505029Actuator · seized(CAN) DURING FINAL APPROACH A/C HAD FLAP FAILURE AT 40 DEGREES.May 5, 2000 · Cndair CL6002B19SDR COMA0060408Flap · failedON APPROACH TO LANDING, FLAP FAIL AT 30 DER TIME 12:00 EST. DEFERRED FLAP FOR RE-INSPECT PER AD 98-20-01.May 4, 2000 · N814CA · Cndair CL6002B19SDR CA000530067Bpsu · failed(CAN) FLAPS FAILED AT 42 DEG ON APPROACH. BITE CHECK CARRIED OUT. RT BPSU REPLACED.May 3, 2000 · Cndair CL6002B19SDR CA000530066Control Unit · failed(CAN) FLAP FAILED, FAULT CLEARED WITH A JOB CARD TO DO A VERIFICATION CHECK OF SYSTEM WAS ISSUED. FECU REPLACED. RIG CHECK CARRIED OUT.May 2, 2000 · Cndair CL6002B19SDR COMA0060398Actuator · seizedFLAPS FAILED AT 40 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP, INBOARD ACTUATOR.May 2, 2000 · N716CA · Cndair CL6002B19SDR DL72L000869Switch · failedA/C AIR TURNBACK WITH PR. NR 6 KRUEGER FLAP FAILED TO RETRACT AFTER DEPARTURE. OPERATED FLAPS SEVERAL TIMES, FOUND NR 6 KRUEGER AND ALL FLAPS OPERATE NORMAL. FOUND L/E FLAP INTRANSIT AMBER LIGHT ON FWD PNL AND ON S/O''S PNL ILLUM. REPLACED THE NR 6 KRUEGERMay 1, 2000 · N502DA · Boeing 727232SDR JBXA0000173Bpsu · failedFLAPS FAILS AT 30 DEGREES ON APPROACH FLAPS FAIL MESSAGE ON EICAS INTO IND. FERRIED TO RDU. REPLACED RT BPSU. RIGGED FLAPS IAW CRJ 27-51-10, OPS CHECK GOOD.Apr 29, 2000 · N584ML · Cndair CL6002B19SDR UPS00232596Support Fitting · corrodedINSPECTION TYPE:C+SI, NR 5 FLAP TRACK FWD SUPPORT FITTING CORRODED. NR 5 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING NR 65-21651.Apr 28, 2000 · N938UP · Boeing 727173CSDR COMA0060393Flap · malfunctionedFLAPS AT 20, FLAPS NOT IN MOTION, FLAPS FAIL MSG, 11;45 EST. COMPLIED WITH EO 27-045AD, INSPECTION OF FLAPS, AND RESET OF SYSTEM. DEFERRED PER GMM 4-3 CAT 1 AND AD 98-20-01.Apr 28, 2000 · N981CA · Cndair CL6002B19SDR UPS00232597Support Fitting · corrodedINSPECTION TYPE:C+SI, NR 4 FLAP TRACK FWD SUPPPORT FITTING CORRODED. NR 4 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING 65-21651.Apr 27, 2000 · N938UP · Boeing 727173CSDR COMA0060387Warning System · activatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Apr 27, 2000 · N975CA · Cndair CL6002B19SDR COMA0060386Warning System · activatedFLAPS FAILED AT 8 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Apr 27, 2000 · N978CA · Cndair CL6002B19SDR MWEA00394Transmitter · inoperativeSTALL WARNING INDICATION FAILURE LIGHT ILLUMINATED CLIMBING THROUGH 25000 FEET AND RE-ILLUMINATED 2 MINUTES AFTER STALL WARNING TEST ON BOTH SYSTEMS. MAINTENANCE REMOVED AND REPLACED FLAP TRANSMITTER AND INDICATOR.Apr 26, 2000 · N216ME · Doug DC932SDR UPS00232614Flap Track · corrodedINSPECTION TYPE:C+SI, SURFACE CORROSION AT AFT O/B ATTACH HOLE FOR NR 5 FLAP TRACK ON RT ML G BEAM. REPAIRED IAW SMRO EO 2000-015-007 UPS ENGINEERING FILE NR 727-57-2154.Apr 25, 2000 · N938UP · Boeing 727173CSDR UPS00232613Flap Track · corrodedINSPECTION TYPE:C+SI, SURFACE CORROSION AT AFT O/B ATTACH HOLE FOR NR 4 FLAP TRACK ON LT ML B BEAM. REPAIR CARRIED OUT IAW SMRO EO 2000-015-006 UPS ENGINEERING FILE NR 727-57-2153.Apr 25, 2000 · N938UP · Boeing 727173CSDR COMA0060382Warning System · activatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Apr 25, 2000 · N784CA · Cndair CL6002B19SDR COMA0060372Flap · out of rigFLAPS FAILED AT 30 DEGREES. ADJUSTED FLAP RIGGING, SYSTEM OPERATION NORMAL.Apr 23, 2000 · N915CA · Cndair CL6002B19SDR UPS00232612Flap Track · corrodedINSPECTION TYPE:C+SI, NR 6 FLAP TRACK AFT MOUNT OUTER SURFACE CORRODED (UPPER.) FOR REPAIR REF SMRO EO 2000-015-009 UPS ENGINEERING FILE NR 727-57-2152.Apr 22, 2000 · N938UP · Boeing 727173CSDR UPS00232611Flap Track · corrodedINSPECTION TYPE:C+SI, NR 3 FLAP TRACK CORROSION AT AFT MOUNT OUT SURFACE FOR REPAIR REF SMRO EO 2000-015-08 UPS ENGINEERING FILE NR 727-57-2151.Apr 22, 2000 · N938UP · Boeing 727173CSDR COMA0060380Pin · missingCONNECTING ROD, LEFT HAND OUTBOARD FLAP, IS NOT ATTACHED. REPLACED BUTE DOOR ACTUATOR ROD PIN.Apr 22, 2000 · N735CA · Cndair CL6002B19SDR UPS00232586Carriage · corrodedINSPECTION TYPE:C+SI, NR 2 FLAP CARRIAGE CORROSION AT SPINDLE INNER BORE AND SMALL BEARING OUTER SURFACE END. CARRIAGE ASSY REPLACED IAW OHM 57-52-11.Apr 21, 2000 · N938UP · Boeing 727173C
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